FR3010147B1 - Suspension isostatique d'un turboreacteur par double support arriere - Google Patents
Suspension isostatique d'un turboreacteur par double support arriereInfo
- Publication number
- FR3010147B1 FR3010147B1 FR1358221A FR1358221A FR3010147B1 FR 3010147 B1 FR3010147 B1 FR 3010147B1 FR 1358221 A FR1358221 A FR 1358221A FR 1358221 A FR1358221 A FR 1358221A FR 3010147 B1 FR3010147 B1 FR 3010147B1
- Authority
- FR
- France
- Prior art keywords
- isostatical
- turboreactor
- suspension
- rear support
- double rear
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 239000000725 suspension Substances 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/04—Mounting of an exhaust cone in the jet pipe
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
- Exhaust Gas After Treatment (AREA)
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1358221A FR3010147B1 (fr) | 2013-08-28 | 2013-08-28 | Suspension isostatique d'un turboreacteur par double support arriere |
BR112016004104-6A BR112016004104B1 (pt) | 2013-08-28 | 2014-08-21 | Cárter de escape equipado para turbo reator de fluxo duplo para aeronave e turbo reator de fluxo duplo |
CN201480052157.7A CN105579672B (zh) | 2013-08-28 | 2014-08-21 | 涡轮喷气发动机的通过后部双支撑的静定悬挂 |
EP14786973.9A EP3039254B1 (fr) | 2013-08-28 | 2014-08-21 | Suspension isostatique d'un turboréacteur par double support arrière |
US14/914,349 US9863273B2 (en) | 2013-08-28 | 2014-08-21 | Isostatic suspension of a turbojet by rear double support |
RU2016108999A RU2682206C2 (ru) | 2013-08-28 | 2014-08-21 | Изостатическая подвеска турбореактивного двигателя при помощи двойного заднего крепления |
PCT/FR2014/052109 WO2015028747A1 (fr) | 2013-08-28 | 2014-08-21 | Suspension isostatique d'un turboréacteur par double support arrière |
CA2921900A CA2921900C (fr) | 2013-08-28 | 2014-08-21 | Suspension isostatique d'un turboreacteur par double support arriere |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1358221A FR3010147B1 (fr) | 2013-08-28 | 2013-08-28 | Suspension isostatique d'un turboreacteur par double support arriere |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3010147A1 FR3010147A1 (fr) | 2015-03-06 |
FR3010147B1 true FR3010147B1 (fr) | 2015-08-21 |
Family
ID=49510354
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1358221A Active FR3010147B1 (fr) | 2013-08-28 | 2013-08-28 | Suspension isostatique d'un turboreacteur par double support arriere |
Country Status (8)
Country | Link |
---|---|
US (1) | US9863273B2 (fr) |
EP (1) | EP3039254B1 (fr) |
CN (1) | CN105579672B (fr) |
BR (1) | BR112016004104B1 (fr) |
CA (1) | CA2921900C (fr) |
FR (1) | FR3010147B1 (fr) |
RU (1) | RU2682206C2 (fr) |
WO (1) | WO2015028747A1 (fr) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB201418396D0 (en) * | 2014-10-17 | 2014-12-03 | Rolls Royce Plc | Gas turbine engine support structures |
FR3051832B1 (fr) * | 2016-05-26 | 2019-09-06 | Safran Aircraft Engines | Procede de fabrication d'un carter d'echappement de turbomachine |
FR3051831B1 (fr) * | 2016-05-26 | 2018-05-18 | Safran Aircraft Engines | Carter d'echappement de turbomachine et son procede de fabrication |
FR3085358B1 (fr) * | 2018-08-31 | 2020-09-25 | Safran Nacelles | Ensemble et procede de manutention d’un ensemble propulsif d’aeronef |
CN109592056B (zh) * | 2018-11-02 | 2022-03-15 | 中国航空工业集团公司西安飞机设计研究所 | 一种加油机吊舱悬挂方法 |
RU199280U1 (ru) * | 2019-03-07 | 2020-08-25 | Публичное акционерное общество "МОТОР СИЧ" | Корпус подвески турбовинтового двигателя |
US11274630B2 (en) * | 2020-02-27 | 2022-03-15 | Rolls-Royce North American Technologies Inc. | Exhaust nozzle with vane support structure for a gas turbine engine |
US11959390B2 (en) * | 2022-08-09 | 2024-04-16 | Pratt & Whitney Canada Corp. | Gas turbine engine exhaust case with blade shroud and stiffeners |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1351414A (fr) | 1962-09-18 | 1964-02-07 | Eastman Kodak Co | Instrument de mesure électrique et ses applications |
US4266741A (en) * | 1978-05-22 | 1981-05-12 | The Boeing Company | Mounting apparatus for fan jet engine having mixed flow nozzle installation |
GB2061389B (en) * | 1979-10-23 | 1983-05-18 | Rolls Royce | Rod installation for a gas turbine engine |
SU849694A1 (ru) * | 1980-03-12 | 1996-09-20 | А.А. Бобух | Устройство для крепления двухконтурного турбореактивного двигателя |
FR2676707B1 (fr) * | 1991-05-23 | 1993-08-13 | Snecma | Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux. |
GB9116986D0 (en) | 1991-08-07 | 1991-10-09 | Rolls Royce Plc | Gas turbine engine nacelle assembly |
US5205513A (en) * | 1991-09-26 | 1993-04-27 | General Electric Company | Method and system for the removal of large turbine engines |
UA62518C2 (en) * | 2003-04-07 | 2005-09-15 | Academician O H Ivchenko State | Rear belt of suspension of gas turbine bypass engine |
FR2907098B1 (fr) | 2006-10-11 | 2010-04-16 | Aircelle Sa | Nacelle pour turboreacteur double flux |
WO2008043903A2 (fr) | 2006-10-11 | 2008-04-17 | Aircelle | Nacelle pour turboréacteur double flux |
FR2924094B1 (fr) | 2007-11-23 | 2010-01-15 | Snecma | Turboreacteur suspendu a un pylone d'aeronef |
FR2928180B1 (fr) | 2008-02-28 | 2010-04-02 | Airbus France | Ensemble moteur pour aeronef comprenant une structure annulaire de transfert d'efforts entourant le carter central d'un turboreacteur. |
US8621874B2 (en) * | 2009-08-25 | 2014-01-07 | Honeywell International Inc. | Turbomachine core coupling assembly |
FR2952126B1 (fr) | 2009-11-04 | 2011-12-23 | Snecma | Turbomachine a double flux pour aeronef, comprenant des moyens structuraux de rigidification du carter central |
ES2391967B1 (es) | 2010-01-14 | 2013-10-10 | Airbus Operations, S.L. | Pilón de soporte de motores de aeronaves. |
FR2975131B1 (fr) | 2011-05-09 | 2015-12-25 | Snecma | Suspension du canal de flux froid d'un turboreacteur par des biellettes et des chapes radiales sur le carter d'echappement |
CA2756914C (fr) * | 2011-11-04 | 2019-01-22 | Pratt & Whitney Canada Corp. | Dispositif d'installation de turbine |
-
2013
- 2013-08-28 FR FR1358221A patent/FR3010147B1/fr active Active
-
2014
- 2014-08-21 EP EP14786973.9A patent/EP3039254B1/fr active Active
- 2014-08-21 CN CN201480052157.7A patent/CN105579672B/zh active Active
- 2014-08-21 US US14/914,349 patent/US9863273B2/en active Active
- 2014-08-21 BR BR112016004104-6A patent/BR112016004104B1/pt active IP Right Grant
- 2014-08-21 WO PCT/FR2014/052109 patent/WO2015028747A1/fr active Application Filing
- 2014-08-21 RU RU2016108999A patent/RU2682206C2/ru active
- 2014-08-21 CA CA2921900A patent/CA2921900C/fr active Active
Also Published As
Publication number | Publication date |
---|---|
WO2015028747A1 (fr) | 2015-03-05 |
EP3039254A1 (fr) | 2016-07-06 |
BR112016004104A2 (fr) | 2017-08-01 |
CN105579672A (zh) | 2016-05-11 |
RU2016108999A3 (fr) | 2018-07-19 |
US20160200443A1 (en) | 2016-07-14 |
FR3010147A1 (fr) | 2015-03-06 |
CN105579672B (zh) | 2018-10-26 |
RU2682206C2 (ru) | 2019-03-15 |
BR112016004104B1 (pt) | 2022-01-04 |
RU2016108999A (ru) | 2017-10-03 |
US9863273B2 (en) | 2018-01-09 |
EP3039254B1 (fr) | 2017-04-19 |
CA2921900C (fr) | 2021-03-16 |
CA2921900A1 (fr) | 2015-03-05 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 3 |
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RM | Correction of a material error |
Effective date: 20160404 |
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PLFP | Fee payment |
Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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CD | Change of name or company name |
Owner name: SNECMA, FR Effective date: 20170713 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |